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Wall-interference assessment in three-dimensional slotted-wall wind tunnelsThe development of the slotted tunnel simulator code and lessons learned from its use are summarized. The high order panel method was selected as the basic procedure for aerodynamic computations. The panel singularities are supplemented by line sources to represent discrete wall slots.
Document ID
19860002773
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kemp, W. B., Jr. (College of William and Mary Williamsburg, VA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.26:176320
NASA-CR-176320
Report Number: NAS 1.26:176320
Report Number: NASA-CR-176320
Accession Number
86N12240
Funding Number(s)
CONTRACT_GRANT: NCC1-69
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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